An envelope detection method based on the first-vibration-mode of bearing vibration Department of Mechanical Engineering, Southern Taiwan University, 1 Nan-Tai Street, Yung Kang City, 710
Trang 1An envelope detection method based on the first-vibration-mode of bearing vibration
Department of Mechanical Engineering, Southern Taiwan University, 1 Nan-Tai Street,
Yung Kang City, 710 Tainan County, Taiwan, ROC Received 29 March 2007; received in revised form 12 September 2007; accepted 23 November 2007
Available online 4 December 2007
Abstract
In this paper, the resonance frequency in the first-vibration-mode of mechanical system is studied and applied in the envelope detection for the bearing vibration The vibration signal of a bearing system is a typical vibration with amplitude modulation Under the assumption of a stepwise function for the envelope signal, the modulated signal could be decom-posed into a sinusoidal function basis at the first-vibration-mode resonance frequency According to the vibration spec-trum, the first-vibration-mode resonance frequency could be initially designated By applying a recursive estimation algorithm, the resonance frequency could be derived more precisely Thus, the envelope signal could be retrieved by esti-mating the coefficients of the function basis with the linear least squares analysis In addition, the vibration signal with noise rejection could be directly reconstructed from the envelope signal According to the experimental study, the envelope detection method for the first-vibration-mode resonance frequency could be effectively applied in the signal processing for the bearing defect diagnosis
Ó 2007 Elsevier Ltd All rights reserved
Keywords: Resonance frequency; Amplitude modulation; Envelope detection; Bearing defect
1 Introduction
The vibration signal of a bearing system is a
typ-ical vibration with amplitude modulation The
high-frequency resonance technique[1]is usually applied
to the mechanical vibrations with amplitude
modu-lation When applying the high-frequency resonance
technique to detect the envelope signal, the
vibra-tion signal is operated through a bandpass filter to derive a single mode vibration and then the envelop-ing transformation is applied to retrieve an envelope signal In the range of the system resonance, this technique takes advantage of the absence of low-fre-quency mechanical noise to demodulate a vibration signal and, therefore, provides a low-frequency envelope signal with a high signal-to-noise ratio
In order to implement the high-frequency resonance technique, the Hilbert transform is often applied in vibration signal demodulation to provide a complex signal Accordingly, the envelope signal could be
0263-2241/$ - see front matter Ó 2007 Elsevier Ltd All rights reserved.
doi:10.1016/j.measurement.2007.11.007
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E-mail address: syt@mail.stut.edu.tw
Measurement 41 (2008) 797–809
www.elsevier.com/locate/measurement
Trang 2obtained from the absolute value of the complex
method in the envelope detection of vibration
signals
Although the high-frequency resonance
tech-nique is widely applied in the envelope detection
of bearing vibration with amplitude modulation, it
is difficult to properly designate the bandpass filter
through which a complete mode vibration could
be filtered There is no guarantee a complete mode
vibration of bearing vibrations could be filtered
through such a bandpass filter Thus, it could
seri-ously distort the envelope signal In addition, when
applying the Hilbert transform in the
high-fre-quency resonance technique for the envelope
detec-tion of vibradetec-tion signals, the computing burden
would be very high
In this paper, a signal processing method and a
recursive estimation algorithm are proposed to
apply in the vibration signal with amplitude
modulation Based on the resonance frequency in
the first-vibration-mode of a mechanical system,
the envelope detection for the vibration signal with
amplitude modulation could be easily and fast
achieved by the linear least squares analysis
According to the vibration spectrum, the resonance
frequency in the first-vibration-mode would be
ini-tially designated A recursive estimation algorithm
would be then proposed to improve the precision
of estimation for the resonance frequency Under
the assumption of a stepwise function for the
enve-lope signal, the vibration signal could be
decom-posed into a sinusoidal function basis at the
resonance frequency Thus, the envelope signal
could be directly retrieved by estimating the
coeffi-cients of the function basis with the linear least
squares analysis Besides, the vibration signal with
noise rejection could be easily reconstructed from
the envelope signal In the experimental study, the
effectiveness of the envelope detection method with
the first-vibration-mode resonance frequency would
be investigated and applied in the bearing defect diagnosis
2 A study on the bearing vibrations 2.1 Amplitude modulation of bearing vibration
In a bearing system, the carrier signal could be a combination of the resonant frequencies of the bear-ing or even of the mechanical system, and thus the vibration signal with amplitude modulation could
be represented as [6–8]
where w(t) is the low-frequency mechanical noise, and the first two summation terms describe the vibrations of defect components and normal compo-nents In the first term of Eq.(1), md is the number of defect, dm(t) depicts the defect impulse train of con-tact and is the modulating signal, qm(t) describes the dimension information of defect and the sensitivity
of striking energy, and alm(t) is the characteristic function of transmission path In the other term, nr
is the number of roller, gn(t) describes the surface functions of normal bearing components with respect to roller n and could also be a modulating signal, qn(t) is the equivalent stiffness of roller n and is a function of the structure stiffness and the oil film stiffness, and aln(t) is the transmission path function which describes the vibration strength excited by roller n For the other variables, rl and
fl are respectively the exponential damping fre-quency and the carrier frefre-quency, and would be the intrinsic characteristics of the system L is the quantity of vibration mode of the system hlm(t) and hln(t) are the initial angles for the amplitude modulation It should be noted that the frequencies
of modulating signal dm(t) and gn(t) would be always much smaller than that of the carrier signal, and the frequencies of modulating signal dm(t) and gn(t) are higher than those of qm(t), alm(t), qn(t) and aln(t)
expanded in frequency band whose center frequency
vðtÞ ¼XL
l¼1
Xmd
m¼1
Z t
1
þXnr
n¼1
Z t
1
!
Trang 3would be at the frequencies of carrier signal This
phenomenon is named as amplitude modulation
Suppose that the impulse responses due to
impacts dm(t) are completely died out in a time
interval between two consecutive impact contacts,
and the resonance frequency flis high The impact
energy due to the surface irregularity gn(t)qn(t)
would be much smaller than that due to the bearing
defects Thus, the second term of Eq (1) could be
neglected Accordingly, the envelope signal of the
lth mode vibration could be written as
elðtÞ ¼Xmd
m¼1
with umðtÞ ¼ er l t0 and t0= mod(t,1/fdm), where wl(t)
is the low-frequency mechanical noise occurring in
thelth vibration mode, mod(t,1/fdm) represents a
residue of t, and fdmis the frequency of impulse train
dm(t) The spectrum for the envelope signal would
show a pattern of the modulating signal frequency
and its harmonics with equal frequency spacing
sidebands which are induced by the frequencies of
qm(t) and alm(t) When applying the high-frequency
resonance technique to detect the envelope signal,
the vibration signal of defect bearing is operated
through a bandpass filter to derive a single vibration
mode and then taking the enveloping
transforma-tion to retrieve an envelope signal However, there
is no guarantee such a signal processing could
de-rived a complete mode vibration Thus, it could
seri-ously distort the envelope signal
2.2 Envelope detection for bearing vibrations
In general, the resonant vibration modes of a
mechanical system would be more than one and
the structure should be strong enough to stably
sup-port the bearing system Thus, the
first-vibration-mode resonance frequency could be high and away
from the range of low-frequency noise In this paper, the first mode vibration is suggested to be fil-tered out in order to reduce the computing burden According to Eq (1), the vibration signal decom-posed into a sinusoidal function basis at the reso-nance frequency f1 in the first-vibration-mode for
a defect bearing could be represented as
v1ðtÞ ¼Xmd m¼1
umðtÞqmðtÞa1mðtÞ cosð2pf1tþ h1mÞ þ w1ðtÞ
¼ aðtÞ cosð2pf1tÞ þ bðtÞ sinð2pf1tÞ þ w1ðtÞ ð3Þ where a(t) and b(t) are the coefficients for the vibra-tion signal v1(t) mapping to a sinusoidal function basis It is noted that the envelope signal would be-come smoother, and the envelope signal could thus
be approximated by a stepwise function Moreover,
it is assumed that every time period of the carrier signal could be divided into two intervals for the envelope detection Accordingly, the above signal could be expressed in a discrete mode
v1ðiÞ ¼ ajcos 2pf1
i
fs
þ bjsin 2pf1
i
fs
þ wj; ð4Þ where i, fsand wjare the sampling point, the sam-pling frequency of the vibration signal, and the vibration noise induced by the vibration noise
wl(t), respectively j is the interval number of the envelope signal Accordingly, the sampling fre-quency fs must be at least 6 times higher than the resonance frequency f1 In addition, an anti-aliasing low-pass filter with the cutoff frequency between f1 and 0.5fsHz should be adopted
As shown in Fig 1, there are more than three equations to solve the unknown coefficients aj, bj and wj If the number of data points is h over the kth half period of the vibration signal v1(t), these points could be expressed in the matrix form
v1ðhðk 1Þ þ 1Þ
v1ðhðk 1Þ þ 2Þ
vlðhkÞ
2
6
6
4
3 7 7
cos 2pf1 ðk1Þþ1
sin 2pf1 ðk1Þþ1
1 cos 2pf1 ðk1Þþ2
sin 2pf1 ðk1Þþ2
1
cos 2pf1hkfs
sin 2pf1hkfs
1
2 6 6 6 6
3 7 7 7 7
ak
bk
wk
2 6 3
Trang 4The above equation could be rewritten as a
simpli-fied expression
½Vkh1¼ ½Mkh3
ak
bk
wk
2 6
3
The solution of the matrix function in three
un-knowns could be obtained in a linear least squares
sense by simple equations
ak
bk
wk
2
6
3
7
5 ¼ ½Mk1h3½Vkh1; for h¼ 3
ak
bk
wk
2
6
3
7
5 ¼ ½M kTh3½Mkh31
½MkTh3½Vkh1; for h > 3
8
>
>
>
>
>
>
>
>
ð7Þ
where T denote the transpose of a matrix
Accord-ingly, the envelope signal in Eq.(2)could be derived
from the following equation:
e1ðjÞ ¼ ffiffiffiffiffiffiffiffiffiffiffiffiffiffiffi
a2
j
q
Moreover, based on the envelope signal, a
recon-structed vibration signal with noise rejection could
be directly derived from
v01ðiÞ ¼ ajcos 2pf1
i f
þ bjsin 2pf1
i f
Accordingly, Eq (9) is the vibration signal corre-sponding to the first mode vibration for the vibra-tion signal
2.3 The designation of the first-vibration-mode resonance frequency for bearing vibrations However, the most important problem in the implementation of the above envelope detection method is how to designate the resonance frequency
in the range of the first-vibration-mode for a vibra-tion signal In general, an easy and feasible way to designate the resonance frequency is to choose a peak
at the frequency ^f1in the range of the first-vibration-mode Thus, the peak frequency ^f1would be an esti-mation of the resonance frequency in the range of the first mode vibration It is very possible that an error
fre-quency Thus, the actual resonance frequency would
be f1¼ ^f1þ Df The vibration signal v0
1ðiÞ of first-vibration-mode decomposed into a sinusoidal func-tion basis at the estimated resonance frequency could
be an estimation of Eq.(9)and would be written as
v01ðiÞ ¼ a0jcos 2p^f1
i
fs
þ b0jsin 2p^f1
i
fs
¼ a0
jcos 2pðf1 Df Þ i
fs
þ b0j
sin 2pðf1 Df Þ i
f
ð10Þ
Time
v l (k 1 )=α1 cos(2πf l k 1 /f s )+β1 sin(2pi f l k 1 /f s ), k 1 =1, 2, ,5
v l (k 1 )=α2 cos(2πf l k 1 /f s )+β2 sin(2πf l k 1 /f s ), k 1 =6, 7, ,10
v
l (k
1 )=α3 cos(2πf
l k
1 /f
s )+β3 sin(2πf
l k
1 /f
s ), k
1 =11, 12, ,15
v
l (k
1 )=α4 cos(2πf
l k
1 /f
s )+β4 sin(2πf
l k
1 /f
s ), k
1 =16, 17, ,20
v l (k 1 )=α3 cos(2πf l k 1 /f s )+β3 sin(2πf l k 1 /f s ), k 1 =21, 22, ,25
Fig 1 The modulated signal for a vibration impact decomposes into a sinusoidal function at its resonant frequency.
Trang 5The above equation could be also rewritten as a
sinusoidal function with fundamental frequency f1,
and be expressed as
v01ðiÞ ¼ a0jcos 2pDf i
fs
b0jsin 2pDf i
fs
i
fs
þ b0jcos 2pDf i
fs
þa0
jsin 2pDf i
fs
sin 2pf1
i
fs
ð11Þ
In comparison between Eqs.(9) and (11), if v0
1ðiÞ ¼
v1ðiÞ the following equations could be derived:
aj¼ a0
fs
b0jsin 2pDf i
fs
ð12:aÞ
bj¼ b0jcos 2pDf i
fs
þ a0jsin 2pDf i
fs
ð12:bÞ
If substituting Eq (12) into Eq (8), the envelope
signal could also be written as
e1ðjÞ ¼ ffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffi
a02
q
It could prove that the envelope signal could be
accurately retrieved, even though, by applying an
estimation of the resonance frequency Thus, an
estimation of the resonance frequency f1 could be
easily derived from the peak in the
first-vibration-mode of the spectrum for the vibration signal Thus,
the proposed envelope detection method would be
capable of applying in practice
Nevertheless, the estimation of the resonance
fre-quency should be accurate enough to apply in Eq.(4)
to derive the envelope signal In the following, a
recursive estimation algorithm for deriving the
first-vibration-mode resonance frequency is proposed:
1 According to the vibration spectrum of the
mea-sured signal, a peak in the first vibration mode
would be initially designated as the resonance
frequency
2 Applying the resonance frequency, the envelope
signal could be derived from the linear least
square analysis, as shown in Eqs (7) and (8)
3 The vibration signal with noise rejection could be
reconstructed from the envelope signal, as shown
in Eq (9)
4 According to the vibration spectrum of the
reconstructed signal derived in Step 3, the peak
would be designated as the resonance frequency
5 Repeat Steps 2–4, until the resonance frequency
is converged
Theoretically, a resonance frequency must exist within the range of first vibration mode on the vibration spectrum The above algorithm should not diverge in estimating the resonance frequency
3 Experimental study
In the following, the applications of the proposed method on the vibration signals of tapered roller bearings (SKF type 32208) are studied The electri-cal-discharge machining method is applied to pro-duce artificial defect on the surface of bearing components which are roller, outer race and inner race The defect sizes are described in theTable 1 The vibration signals are measured on the housing
of the test bearing The measured direction is radial
to the shaft
Under different running speeds, the proposed envelope detection method is applied and the results are shown inFigs 2–4, respectively According to Figs 2a, 3a and 4a, the passband frequencies are similar under different running speeds except that the amplitude is increased, especially at the high-fre-quency band, with the running speed There could
be four resonance modes with the passband fre-quencies from 1 to 3 kHz, 3 to 5 kHz, 6 to 8 kHz and 8 to 10 kHz, respectively In addition, it is noted that the four resonance modes are also similar under different types of bearing defect Thus, the cutoff frequency of the low-pass filter for deriving the first-vibration-mode of bearing vibrations could be designated to be 3 kHz and a sampling rate 18
4b, the initial values designated for the first-vibra-tion-mod resonance frequencies are 2386, 2487 and 1671 Hz, respectively By applying the recursive estimation method in the estimation of the reso-nance frequencies, the vibration spectra are shown
in Figs 2c, 3c and 4c with at the first-vibration-mod resonance frequencies at 2386, 2487 and
2519 Hz, respectively It is noted that the resonance
Table 1 Defect sizes of defective bearings Defect type Defect size (length width depth) Roller defect 16 mm 0.15 mm 0.1 mm Outer-race defect 14 mm 0.15 mm 0.1 mm Inner-race defect 18.5 mm 0.15 mm 0.1 mm
Trang 6recursive iterations In addition, the vibration
spec-tra shown inFigs 2c, 3c and 4cfor the reconstructed
signals are almost the same as those shown inFigs
2b, 3b and 4b, respectively, in the passband from
1.5 to 3 kHz for the measured signals
From the theoretical study, it is assumed that the first mode vibration should be filtered through an anti-aliasing low-pass filter According to the above experimental study, it would prove that the first vibration mode of vibration signal could be filtered
0 0.1 0.2 0.3
Frequency (Hz)
a
1st vibration mode
2nd vibration mode
3rd vibration mode
4th vibration mode
0 500 1000 1500 2000 2500 3000 3500 4000 4500 5000 0
0.1 0.2
*
0 500 1000 1500 2000 2500 3000 3500 4000 4500 5000 0
0.1 0.2
Frequency (Hz)
* :the initial designated resonance frequency b
c
* :the first-vibration-mode resonance frequency
*
Fig 2 The vibration spectra for the roller defect bearing running at 800 rpm (a) For the vibration signal with a passband from 0 to
12 kHz, (b) for the vibration signal with a passband from 0 to 3 kHz, (c) for the reconstructed signal derived from the envelope signal.
Trang 7through an anti-aliasing low-pass filter with the
cut-off frequency at 3 kHz Thus, the characteristics of
the vibration signal in the first vibration mode could
be very well represented by the reconstructed signal
in Eq (9)
In the following,Fig 5shows the effectiveness of the proposed method on the envelope detection for
a roller defect bearing at the running speed
1600 rpm Fig 5a–c shows the measured vibration signal, the retrieved envelope signal from Fig 5a,
0 1 2 3 4 5
Frequency (Hz)
a
1st vibration mode
2nd vibration mode
3rd vibration mode
4th vibration mode
0 500 1000 1500 2000 2500 3000 3500 4000 4500 5000 0
0.5 1 1.5
0 500 1000 1500 2000 2500 3000 3500 4000 4500 5000 0
0.5 1 1.5
Frequency (Hz)
* :the initial designated resonance frequency
*
b
* :the first-vibration-mode resonance frequency
*
c
Fig 3 The vibration spectra for the roller defect bearing running at 1600 rpm (a) For the vibration signal with a passband from 0 to
12 kHz, (b) for the vibration signal with a passband from 0 to 3 kHz, (c) for the reconstructed signal derived from the envelope signal.
Trang 8and the reconstructed signal derived fromFig 5b,
respectively For the purpose of comparison, the
envelope signal derived from the high-frequency
resonant technique with the passband from 1 to
Fig 5d,Fig 5b shows a smoother signal with lower noise In addition,Fig 6a and b show the envelope spectra for the envelope signal in Fig 5b and d, respectively The envelope spectra are also similar
0 3 6 9
Frequency (Hz)
a
1st vibration mode
2nd vibration mode
4th vibration mode
3rd vibration mode
0 500 1000 1500 2000 2500 3000 3500 4000 4500 5000 0
1 2 3
*
0 500 1000 1500 2000 2500 3000 3500 4000 4500 5000 0
1 2 3
Frequency (Hz)
* :the initial designated resonance frequency
b
* :the first-vibration-mode resonance frequency c
*
Fig 4 The vibration spectra for the roller defect bearing running at 2400 rpm (a) For the vibration signal with a passband from 0 to
12 kHz, (b) for the vibration signal with a passband from 0 to 3 kHz, (c) for the reconstructed signal derived from the envelope signal.
Trang 9frequency at 154 Hz for the roller defect Thus, it
would prove that the proposed method could be
effective in the envelope detection for the bearing vibration
0 0.01 0.02 0.03 0.04 0.05 0.06 0.07 0.08 0.09 0.1 -2
0 2
0 0.01 0.02 0.03 0.04 0.05 0.06 0.07 0.08 0.09 0.1 0
0.5 1
0 0.01 0.02 0.03 0.04 0.05 0.06 0.07 0.08 0.09 0.1 -2
0 2
0 0.01 0.02 0.03 0.04 0.05 0.06 0.07 0.08 0.09 0.1 0
0.5 1
Time (sec)
a
b
c
d
Fig 5 (a) The measured vibration signal for the roller defect bearing running at 1600 rpm, (b) the envelope signal of (a) in the first vibration mode, (c) the reconstructed signal from (b), (d) the envelope signal derived from the high-frequency resonance technique.
0 2 4 6 8
0 3 6 9 12
Frequency (Hz)
a
b
Fig 6 The envelope spectra for a roller defect bearing running at 1600 rpm (a) By applying the envelope detection with the first-vibration-mode resonance frequency, (b) by applying the high frequency resonance technique with a filtering passband from 1 to 3 kHz.
Trang 10Similar to Figs 6–8 show the envelope spectra
with the characteristic frequency at 190 Hz and
266 Hz for the outer-race defect bearing and the inner-race defect bearing, respectively It is found
0 2 4 6 8 10
0 2 4 6 8 10
Frequency (Hz)
a
b
Fig 7 The envelope spectra for a outer-race defect bearing running at 1600 rpm (a) By applying the envelope detection with the first-vibration-mode resonance frequency (b) By applying the high frequency resonance technique with a filtering passband from 1 to 3 kHz.
0 1 2
0 1 2
Frequency (Hz)
a
b
Fig 8 The envelope spectra for a inner-race defect bearing running at 1600 rpm (a) By applying the envelope detection with the first-vibration-mode resonance frequency (b) By applying the high frequency resonance technique with a filtering passband from 1 to 3 kHz.